CN105526891A - Turbine shell assembly test-bed - Google Patents
Turbine shell assembly test-bed Download PDFInfo
- Publication number
- CN105526891A CN105526891A CN201610006194.5A CN201610006194A CN105526891A CN 105526891 A CN105526891 A CN 105526891A CN 201610006194 A CN201610006194 A CN 201610006194A CN 105526891 A CN105526891 A CN 105526891A
- Authority
- CN
- China
- Prior art keywords
- turbine
- plate
- air cylinder
- cylinder group
- fixed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000000463 material Substances 0.000 claims abstract description 8
- 230000008030 elimination Effects 0.000 claims description 21
- 238000003379 elimination reaction Methods 0.000 claims description 21
- 235000004443 Ricinus communis Nutrition 0.000 claims description 9
- 240000000528 Ricinus communis Species 0.000 claims description 3
- 238000001514 detection method Methods 0.000 abstract description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000003908 quality control method Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
Abstract
The invention relates to a turbine shell assembly test-bed, belonging to the field of automobile part assembly detection. The turbine shell assembly test-bed comprises a rack, a display, an electric control cabinet, an industrial control cabinet, a scan gun, a button box, a material shelf, a turbine angle adjusting mechanism, a turbine measuring mechanism, a turbine angle positioning mechanism and a turbine eliminating mechanism; the rack comprises an upper rack and a lower rack, the display is fixed on the upper rack, the electric control cabinet is connected to the back of the lower rack, the industrial control cabinet is arranged in the lower rack, the scan gun and the button box are arranged at the front end of the lower rack, and the material shelf is fixed on the lower rack; the turbine angle adjusting mechanism, the turbine measuring mechanism and the turbine eliminating mechanism are all fixed on the lower rack; and the turbine angle positioning mechanism is connected with the turbine angle adjusting mechanism. The turbine shell assembly test-bed is reasonable in structure, and can reduce the labor strength and the labor cost, detect a turbine shell accurately and improve the production quality and the assembly efficiency.
Description
Technical field
The present invention relates to a kind of monitor station, especially relate to a kind of turbine case assembly test table, it is applied in turbosupercharger Assembly and inspect line, and it belongs to automobile component assembling detection field.
Background technology
Along with scientific-technical progress and economic development, turbosupercharger are more and more extensive in engineer applied, turbosupercharger assembling at present basic manual assembly or the indivedual operation of adopting only is assembled with special plane, need when assembly manipulation constantly to carry parts, semifinished or finished goods, need again to carry parts, semifinished or finished goods in order to detect, also, labour intensity be large, efficiency is low, difficult quality control.
The monitor station of prior art, detects unreasonable and range of application is little, has defective place not easily to discover, and is unfavorable for the overall manufacture level improving assembly technology equipment.
Publication date is on 09 24th, 2014, and publication number is in the Chinese patent of 104061833A, discloses the patent of invention that a kind of name is called " a kind of turbocharger turbine shell position detecting tool ".This patent comprises detection platform, and the side of detection platform is provided with wedge pair by bearing, and cammed surface and the turbine case air inlet actinal surface to be detected of wedge pair fit, and join
The inner side of closing described turbine case air intake opening is provided with adjustable ejector rod in described detection platform, and described detection platform is provided with Extendible knockout pin relative to the opposite side of wedge pair.Turbocharger turbine shell position detecting tool Problems existing in this patent prior art, but can not comprehensively assemble turbine case and detect, therefore still there is above-mentioned defect in it.
Summary of the invention
The object of the invention is to overcome above shortcomings in prior art, and a kind of reasonable in design is provided, can labour intensity be reduced, reduce cost of labor, accurate to the detection of turbine case, improve the turbine case assembly test table of the quality of production and efficiency of assembling.
The present invention's adopted technical scheme that solves the problem is: this turbine case assembly test table, comprise stand, display, electrical control cubicles, industry control rack, scanner, button box and material frame, stand comprises upper stage and lower stage, display is fixed in upper stage, electrical control cubicles is connected to the rear of lower stage, industry control rack is arranged in lower stage, scanner and button box are all arranged on the front end of lower stage, material frame is fixed in lower stage, it is characterized in that: also comprise turbine angle-adjusting mechanism, turbine measuring mechanism, turbine angle positioning and turbine eliminating machine, described turbine angle-adjusting mechanism, turbine measuring mechanism and turbine eliminating machine are all fixed in lower stage, turbine angle positioning is connected with turbine angle-adjusting mechanism, turbine angle-adjusting mechanism comprises reductor, electromagnetic clutch, servomotor, index plate, turbine support plate, turbine Timing Belt, turbine base and sleeve, turbine base is fixed on index plate, turbine support plate is connected to the bottom of index plate, electromagnetic clutch is connected with turbine support plate, reductor is connected with electromagnetic clutch, and servomotor is connected with reductor, and turbine Timing Belt coordinates with electromagnetic clutch, sleeve is positioned at electromagnetic clutch outside, and this sleeve is connected with turbine support plate, turbine measuring mechanism comprises turbine and measures mounting base, top board measured by turbine, guide rails assembling plate measured by turbine, side installing plate, turbine slide rail skateboard component one, turbine slide rail skateboard component two, turbine air cylinder group one, turbine air cylinder group two, turbine air cylinder group three, turbine air cylinder group four and measuring mechanism cylinder, turbine is measured mounting base and turbine and is measured top board and measure guide rails assembling plate by turbine and be connected, the both ends of the surface that top board measured by turbine are all connected with side installing plate, one side and the turbine of side installing plate are measured mounting base and are connected, another side and the turbine of this side installing plate are measured top board and are connected, turbine slide rail skateboard component one and turbine slide rail skateboard component two are all fixed on turbine and measure on guide rails assembling plate, turbine air cylinder group one and turbine air cylinder group two are all fixed on turbine and measure on top board, turbine air cylinder group one is connected with turbine slide rail skateboard component one, turbine air cylinder group two is connected with turbine slide rail skateboard component two, turbine air cylinder group three and turbine air cylinder group four are all fixed on turbine and measure on mounting base, turbine air cylinder group three and turbine air cylinder group four lay respectively at the below of turbine slide rail skateboard component one and turbine slide rail skateboard component two, measuring mechanism cylinder is arranged on turbine slide rail skateboard component one, rational in infrastructure, can labour intensity be reduced, reduce cost of labor, accurate to the detection of turbine case, improve the quality of production and efficiency of assembling.
As preferably, turbine angle positioning of the present invention comprises turbine sliding-rail sliding assembly, turbine location slide plate, turbine location-plate, turbine position block, turbine fixed head, turbine slide block, turbine guide pipe, turbine positioning and guiding axle, turbine location top board, valve pin and turbine position fixing handle, turbine location slide plate is connected with turbine sliding-rail sliding assembly, one end of turbine location slide plate is connected with turbine location-plate, the other end of this turbine location slide plate is connected with turbine position block, turbine fixed head is fixed on the slide plate of turbine location, turbine slide block is positioned at the top of turbine location slide plate, turbine guide pipe is two, these two turbine guide pipes all with the cross-under of turbine slide block, the end face of two turbine guide pipes is connected with turbine fixed head and turbine position block respectively, turbine location top board is positioned at the top of turbine slide block, turbine positioning and guiding axle is two, turbine location top board is connected with turbine slide block by two turbine positioning and guiding axles, valve pin is connected with turbine slide block, turbine position fixing handle is fixed on the top board of turbine location.
As preferably, turbine eliminating machine of the present invention comprises turbine and eliminates base plate, guide rail guide block part eliminated by turbine, slide plate eliminated by turbine, main body eliminated by turbine, eliminate back up pad, eliminate supporting seat, eliminate guide plate, eliminate the axis of guide, top chock, lifting shaft and handwheel, turbine elimination guide rail guide block part is eliminated base plate with turbine and is connected, turbine elimination slide plate is eliminated guide rail guide block part with turbine and is connected, turbine is eliminated main body and is fixed on turbine elimination slide plate, eliminate back up pad and be positioned at the top that slide plate eliminated by turbine, eliminating supporting seat is fixed in elimination back up pad, eliminate guide plate to be connected with elimination supporting seat by eliminating the axis of guide, top chock and turbine are eliminated main body and are connected, handwheel is arranged on top chock, lifting shaft is arranged on top chock.
As preferably, turbine measuring mechanism of the present invention also comprises measuring mechanism sensor, and turbine air cylinder group three and turbine air cylinder group four are provided with measuring mechanism sensor.
As preferably, turbine case assembly test table of the present invention also comprises illuminating lamp and tower lamp, and this illuminating lamp and tower lamp are installed in upper stage; Operating environment is become clear.
As preferably, turbine case assembly test table of the present invention also comprises display bracket, and display is fixed by this display bracket and upper stage.
As preferably, turbine case assembly test table of the present invention also comprises hook, and described hook is suspended in upper stage; For hanging tool.
As preferably, turbine case assembly test table of the present invention also comprises castor, and this castor is four, and four castors are all arranged on the bottom surface of lower stage; Be convenient to carrying and move.
The present invention compared with prior art, has the following advantages and effect: rational in infrastructure, can reduce labour intensity, reduces cost of labor, accurate to the detection of turbine case, improves the quality of production and efficiency of assembling, is beneficial to the overall manufacture level improving assembly technology equipment.
Accompanying drawing explanation
Fig. 1 is the one-piece construction schematic diagram of the embodiment of the present invention.
Fig. 2 is the structural representation of turbine angle-adjusting mechanism in the embodiment of the present invention.
Fig. 3 is the structural representation of turbine measuring mechanism in the embodiment of the present invention.
Fig. 4 is the structural representation of turbine angle positioning in the embodiment of the present invention.
Fig. 5 is the structural representation of turbine eliminating machine in the embodiment of the present invention.
Fig. 6 is the structural representation of upper stage in the embodiment of the present invention.
Fig. 7 is the structural representation of lower stage in the embodiment of the present invention.
In figure: stand 1, turbine angle-adjusting mechanism 2, turbine measuring mechanism 3, turbine angle positioning 4, turbine eliminating machine 5, display 6, electrical control cubicles 7, industry control rack 8, scanner 9, button box 10, material frame 11, illuminating lamp 12, tower lamp 13, hook 14, display bracket 15, castor 16, upper stage 101, lower stage 102, reductor 201, electromagnetic clutch 202, servomotor 203, index plate 204, turbine support plate 205, turbine Timing Belt 206, turbine base 207, sleeve 208, mounting base 301 measured by turbine, top board 302 measured by turbine, guide rails assembling plate 303 measured by turbine, side installing plate 304, turbine slide rail skateboard component 1, turbine slide rail skateboard component 2 306, turbine air cylinder group 1, turbine air cylinder group 2 308, turbine air cylinder group 3 309, turbine air cylinder group 4 310, measuring mechanism cylinder 311, measuring mechanism sensor 312, turbine sliding-rail sliding assembly 401, turbine location slide plate 402, turbine location-plate 403, turbine position block 404, turbine fixed head 405, turbine slide block 406, turbine guide pipe 407, turbine positioning and guiding axle 408, turbine location top board 409, valve pin 410, turbine position fixing handle 411, base plate 501 eliminated by turbine, guide rail guide block part 502 eliminated by turbine, slide plate 503 eliminated by turbine, main body 504 eliminated by turbine, eliminate back up pad 505, eliminate supporting seat 506, eliminate guide plate 507, eliminate the axis of guide 508, top chock 509, lifting shaft 510, handwheel 511.
Embodiment
Below in conjunction with accompanying drawing, also by embodiment, the present invention is described in further detail, and following examples are explanation of the invention and the present invention is not limited to following examples.
Embodiment.
See Fig. 1 to Fig. 7, the turbine case assembly test table in the present embodiment mainly comprises stand 1, turbine angle-adjusting mechanism 2, turbine measuring mechanism 3, turbine angle positioning 4 and turbine eliminating machine 5.
Stand 1 in the present embodiment comprises upper stage 101 and lower stage 102, display 6 is fixed in upper stage 101, electrical control cubicles 7 is connected to the rear of lower stage 102, industry control rack 8 is arranged in lower stage 102, scanner 9 and button box 10 are all arranged on the front end of lower stage 102, material frame 11 is fixed in lower stage 102, and turbine angle-adjusting mechanism 2, turbine measuring mechanism 3 and turbine eliminating machine 5 are all fixed in lower stage 102, and turbine angle positioning 4 is connected with turbine angle-adjusting mechanism 2.
Turbine angle-adjusting mechanism 2 in the present embodiment comprises reductor 201, electromagnetic clutch 202, servomotor 203, index plate 204, turbine support plate 205, turbine Timing Belt 206, turbine base 207 and sleeve 208, turbine base 207 is fixed on index plate 204, turbine support plate 205 is connected to the bottom of index plate 204, electromagnetic clutch 202 is connected with turbine support plate 205, reductor 201 is connected with electromagnetic clutch 202, servomotor 203 is connected with reductor 201, turbine Timing Belt 206 coordinates with electromagnetic clutch 202, it is outside that sleeve 208 is positioned at electromagnetic clutch 202, this sleeve 208 is connected with turbine support plate 205, during work, servomotor 203 drives index plate 204 to turn to corresponding position, carry out screw assembling, altogether locate six positions, fill six screws.
Turbine measuring mechanism 3 in the present embodiment comprises turbine and measures mounting base 301, turbine measurement top board 302, turbine measurement guide rails assembling plate 303, side installing plate 304, turbine slide rail skateboard component 1, turbine slide rail skateboard component 2 306, turbine air cylinder group 1, turbine air cylinder group 2 308, turbine air cylinder group 3 309, turbine air cylinder group 4 310 and measuring mechanism cylinder 311.
Turbine in the present embodiment is measured mounting base 301 and turbine and is measured top board 302 and measure guide rails assembling plate 303 by turbine and be connected, the both ends of the surface that top board 302 measured by turbine are all connected with side installing plate 304, one side and the turbine of side installing plate 304 are measured mounting base 301 and are connected, another side and the turbine of this side installing plate 304 are measured top board 302 and are connected, turbine slide rail skateboard component 1 and turbine slide rail skateboard component 2 306 are all fixed on turbine and measure on guide rails assembling plate 303, turbine air cylinder group 1 and turbine air cylinder group 2 308 are all fixed on turbine and measure on top board 302, turbine air cylinder group 1 is connected with turbine slide rail skateboard component 1, turbine air cylinder group 2 308 is connected with turbine slide rail skateboard component 2 306, turbine air cylinder group 3 309 and turbine air cylinder group 4 310 are all fixed on turbine and measure on mounting base 301, turbine air cylinder group 3 309 and turbine air cylinder group 4 310 lay respectively at the below of turbine slide rail skateboard component 1 and turbine slide rail skateboard component 2 306, measuring mechanism cylinder 311 is arranged on turbine slide rail skateboard component 1.
Turbine angle positioning 4 in the present embodiment comprises turbine sliding-rail sliding assembly 401, turbine location slide plate 402, turbine location-plate 403, turbine position block 404, turbine fixed head 405, turbine slide block 406, turbine guide pipe 407, turbine positioning and guiding axle 408, turbine location top board 409, valve pin 410 and turbine position fixing handle 411.
Turbine location slide plate 402 in the present embodiment is connected with turbine sliding-rail sliding assembly 401, one end of turbine location slide plate 402 is connected with turbine location-plate 403, the other end of this turbine location slide plate 402 is connected with turbine position block 404, turbine fixed head 405 is fixed on the slide plate 402 of turbine location, turbine slide block 406 is positioned at the top of turbine location slide plate 402, turbine guide pipe 407 is two, these two turbine guide pipes 407 all with turbine slide block 406 cross-under, the end face of two turbine guide pipes 407 is connected with turbine fixed head 405 and turbine position block 404 respectively, turbine location top board 409 is positioned at the top of turbine slide block 406, turbine positioning and guiding axle 408 is two, turbine location top board 409 is connected with turbine slide block 406 by two turbine positioning and guiding axles 408, valve pin 410 is connected with turbine slide block 406, turbine position fixing handle 411 is fixed on the top board 409 of turbine location.
Turbine eliminating machine 5 in the present embodiment comprises turbine to be eliminated base plate 501, turbine elimination guide rail guide block part 502, turbine elimination slide plate 503, turbine elimination main body 504, elimination back up pad 505, eliminates supporting seat 506, elimination guide plate 507, the elimination axis of guide 508, top chock 509, lifting shaft 510 and handwheel 511.
Turbine elimination guide rail guide block part 502 in the present embodiment is eliminated base plate 501 with turbine and is connected, turbine elimination slide plate 503 is eliminated guide rail guide block part 502 with turbine and is connected, turbine is eliminated main body 504 and is fixed on turbine elimination slide plate 503, eliminate back up pad 505 and be positioned at the top that slide plate 503 eliminated by turbine, eliminating supporting seat 506 is fixed in elimination back up pad 505, eliminate guide plate 507 to be connected with elimination supporting seat 506 by eliminating the axis of guide 508, top chock 509 and turbine are eliminated main body 504 and are connected, handwheel 511 is arranged on top chock 509, lifting shaft 510 is arranged on top chock 509.
Turbine measuring mechanism 3 in the present embodiment also comprises measuring mechanism sensor 312, and turbine air cylinder group 3 309 and turbine air cylinder group 4 310 are provided with measuring mechanism sensor 312.
Illuminating lamp 12 in the present embodiment and tower lamp 13 are installed in upper stage 101, and display 6 is fixed by this display bracket 15 and upper stage 101, and hook 14 is suspended in upper stage 101.
Castor 16 in the present embodiment is four, and four castors 16 are all arranged on the bottom surface of lower stage 102.
By above-mentioned elaboration, those skilled in the art can implement.
In addition, it should be noted that, the specific embodiment described in this instructions, the shape, institute's title of being named etc. of its parts and components can be different, and the above content described in this instructions is only to structure example of the present invention explanation.The equivalence change that structure, feature and the principle of all foundations described in inventional idea of the present invention are done or simple change, be included in the protection domain of patent of the present invention.Those skilled in the art can make various amendment or supplement or adopt similar mode to substitute to described specific embodiment; only otherwise depart from structure of the present invention or surmount this scope as defined in the claims, protection scope of the present invention all should be belonged to.
Claims (8)
1. a turbine case assembly test table, comprise stand, display, electrical control cubicles, industry control rack, scanner, button box and material frame, stand comprises upper stage and lower stage, display is fixed in upper stage, electrical control cubicles is connected to the rear of lower stage, industry control rack is arranged in lower stage, scanner and button box are all arranged on the front end of lower stage, material frame is fixed in lower stage, it is characterized in that: also comprise turbine angle-adjusting mechanism, turbine measuring mechanism, turbine angle positioning and turbine eliminating machine, described turbine angle-adjusting mechanism, turbine measuring mechanism and turbine eliminating machine are all fixed in lower stage, turbine angle positioning is connected with turbine angle-adjusting mechanism, turbine angle-adjusting mechanism comprises reductor, electromagnetic clutch, servomotor, index plate, turbine support plate, turbine Timing Belt, turbine base and sleeve, turbine base is fixed on index plate, turbine support plate is connected to the bottom of index plate, electromagnetic clutch is connected with turbine support plate, reductor is connected with electromagnetic clutch, and servomotor is connected with reductor, and turbine Timing Belt coordinates with electromagnetic clutch, sleeve is positioned at electromagnetic clutch outside, and this sleeve is connected with turbine support plate, turbine measuring mechanism comprises turbine and measures mounting base, top board measured by turbine, guide rails assembling plate measured by turbine, side installing plate, turbine slide rail skateboard component one, turbine slide rail skateboard component two, turbine air cylinder group one, turbine air cylinder group two, turbine air cylinder group three, turbine air cylinder group four and measuring mechanism cylinder, turbine is measured mounting base and turbine and is measured top board and measure guide rails assembling plate by turbine and be connected, the both ends of the surface that top board measured by turbine are all connected with side installing plate, one side and the turbine of side installing plate are measured mounting base and are connected, another side and the turbine of this side installing plate are measured top board and are connected, turbine slide rail skateboard component one and turbine slide rail skateboard component two are all fixed on turbine and measure on guide rails assembling plate, turbine air cylinder group one and turbine air cylinder group two are all fixed on turbine and measure on top board, turbine air cylinder group one is connected with turbine slide rail skateboard component one, turbine air cylinder group two is connected with turbine slide rail skateboard component two, turbine air cylinder group three and turbine air cylinder group four are all fixed on turbine and measure on mounting base, turbine air cylinder group three and turbine air cylinder group four lay respectively at the below of turbine slide rail skateboard component one and turbine slide rail skateboard component two, measuring mechanism cylinder is arranged on turbine slide rail skateboard component one.
2. turbine case assembly test table according to claim 1, it is characterized in that: described turbine angle positioning comprises turbine sliding-rail sliding assembly, turbine location slide plate, turbine location-plate, turbine position block, turbine fixed head, turbine slide block, turbine guide pipe, turbine positioning and guiding axle, turbine location top board, valve pin and turbine position fixing handle, turbine location slide plate is connected with turbine sliding-rail sliding assembly, one end of turbine location slide plate is connected with turbine location-plate, the other end of this turbine location slide plate is connected with turbine position block, turbine fixed head is fixed on the slide plate of turbine location, turbine slide block is positioned at the top of turbine location slide plate, turbine guide pipe is two, these two turbine guide pipes all with the cross-under of turbine slide block, the end face of two turbine guide pipes is connected with turbine fixed head and turbine position block respectively, turbine location top board is positioned at the top of turbine slide block, turbine positioning and guiding axle is two, turbine location top board is connected with turbine slide block by two turbine positioning and guiding axles, valve pin is connected with turbine slide block, turbine position fixing handle is fixed on the top board of turbine location.
3. turbine case assembly test table according to claim 1, it is characterized in that: described turbine eliminating machine comprises turbine and eliminates base plate, guide rail guide block part eliminated by turbine, slide plate eliminated by turbine, main body eliminated by turbine, eliminate back up pad, eliminate supporting seat, eliminate guide plate, eliminate the axis of guide, top chock, lifting shaft and handwheel, turbine elimination guide rail guide block part is eliminated base plate with turbine and is connected, turbine elimination slide plate is eliminated guide rail guide block part with turbine and is connected, turbine is eliminated main body and is fixed on turbine elimination slide plate, eliminate back up pad and be positioned at the top that slide plate eliminated by turbine, eliminating supporting seat is fixed in elimination back up pad, eliminate guide plate to be connected with elimination supporting seat by eliminating the axis of guide, top chock and turbine are eliminated main body and are connected, handwheel is arranged on top chock, lifting shaft is arranged on top chock.
4. turbine case assembly test table according to claim 1, is characterized in that: described turbine measuring mechanism also comprises measuring mechanism sensor, and turbine air cylinder group three and turbine air cylinder group four are provided with measuring mechanism sensor.
5. turbine case assembly test table according to claim 1, is characterized in that: described turbine case assembly test table also comprises illuminating lamp and tower lamp, and this illuminating lamp and tower lamp are installed in upper stage.
6. turbine case assembly test table according to claim 1, is characterized in that: described turbine case assembly test table also comprises display bracket, and display is fixed by this display bracket and upper stage.
7. turbine case assembly test table according to claim 1, is characterized in that: described turbine case assembly test table also comprises hook, and described hook is suspended in upper stage.
8. turbine case assembly test table according to claim 1, is characterized in that: described turbine case assembly test table also comprises castor, and this castor is four, and four castors are all arranged on the bottom surface of lower stage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610006194.5A CN105526891B (en) | 2016-01-07 | 2016-01-07 | Turbine case assembly test table |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610006194.5A CN105526891B (en) | 2016-01-07 | 2016-01-07 | Turbine case assembly test table |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105526891A true CN105526891A (en) | 2016-04-27 |
| CN105526891B CN105526891B (en) | 2017-12-01 |
Family
ID=55769267
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610006194.5A Active CN105526891B (en) | 2016-01-07 | 2016-01-07 | Turbine case assembly test table |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105526891B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108072407A (en) * | 2017-12-05 | 2018-05-25 | 常州中车汽车零部件有限公司 | Turbine case flow-paths inspection system and method |
| CN108709528A (en) * | 2018-05-17 | 2018-10-26 | 江南大学 | A kind of vehicle turbine shell cubing |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201516547U (en) * | 2009-05-07 | 2010-06-30 | 无锡康明斯涡轮增压技术有限公司 | Automatic angle-adjusting device |
| EP2650493A2 (en) * | 2012-04-12 | 2013-10-16 | General Electric Company | Turbine shell displacement monitoring system |
| CN203918392U (en) * | 2014-05-09 | 2014-11-05 | 杭州高品自动化设备有限公司 | Cooler core end cap assembling special plane |
| CN204154296U (en) * | 2014-10-31 | 2015-02-11 | 无锡麦铁精密机械制造有限公司 | A kind of structure of comprehensive check tool of turbine case |
-
2016
- 2016-01-07 CN CN201610006194.5A patent/CN105526891B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201516547U (en) * | 2009-05-07 | 2010-06-30 | 无锡康明斯涡轮增压技术有限公司 | Automatic angle-adjusting device |
| EP2650493A2 (en) * | 2012-04-12 | 2013-10-16 | General Electric Company | Turbine shell displacement monitoring system |
| CN203918392U (en) * | 2014-05-09 | 2014-11-05 | 杭州高品自动化设备有限公司 | Cooler core end cap assembling special plane |
| CN204154296U (en) * | 2014-10-31 | 2015-02-11 | 无锡麦铁精密机械制造有限公司 | A kind of structure of comprehensive check tool of turbine case |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108072407A (en) * | 2017-12-05 | 2018-05-25 | 常州中车汽车零部件有限公司 | Turbine case flow-paths inspection system and method |
| CN108072407B (en) * | 2017-12-05 | 2021-03-02 | 常州中车汽车零部件有限公司 | Turbine shell flow passage detection system and method |
| CN108709528A (en) * | 2018-05-17 | 2018-10-26 | 江南大学 | A kind of vehicle turbine shell cubing |
| CN108709528B (en) * | 2018-05-17 | 2019-09-03 | 江南大学 | A kind of vehicle turbine shell cubing |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105526891B (en) | 2017-12-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105458672B (en) | Core body assembly bench | |
| CN106441706B (en) | It is integrated in the center mass measuring device of more size slender bodies assembly bench | |
| CN105783837A (en) | Third-generation automobile hub bearing axial clearance automatic measuring device | |
| CN105526891A (en) | Turbine shell assembly test-bed | |
| CN105509664A (en) | Performer adjustment detection bench | |
| CN205352334U (en) | Assembly of turbine shell detects platform | |
| CN204788144U (en) | Bent shaft detection device | |
| CN105674928B (en) | Rotor elongation and bounce detection table | |
| CN205352454U (en) | Axial float and leak testing platform | |
| CN203382393U (en) | Lifting appliance detection device | |
| CN105526970B (en) | Axial float and leak-testing platform | |
| CN105537896B (en) | Extend measuring mechanism | |
| CN205373671U (en) | Rotor elongation and detection platform of beating | |
| CN204188146U (en) | Body in white cubing testing agency | |
| CN209387277U (en) | A kind of device for fast detecting of compressor pulley end face and clutch cover | |
| CN107091605A (en) | A kind of practical measuring instrument of crankshaft end-face glitch detection | |
| CN203918427U (en) | Intelligent Selection pad machine | |
| CN202092554U (en) | Dimension testing fixture for engine valve from valve line to rod end face | |
| CN105466639A (en) | Rotor smoothness assembly leakage table | |
| CN206583393U (en) | A kind of stamping parts of automobile detection means | |
| CN204479048U (en) | A kind of pick-up unit of sleeve | |
| CN205352330U (en) | Executor adjustment detects platform | |
| CN203259088U (en) | Integrated measuring instrument for form and location tolerance of intake-exhaust valve | |
| CN201724635U (en) | Diesel engine body support detecting apparatus | |
| CN209359948U (en) | PLC machine electricity experimental bench |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Turbine housing assembly test bench Effective date of registration: 20211206 Granted publication date: 20171201 Pledgee: Hangzhou High-tech Financing Guarantee Co.,Ltd. Pledgor: HANGZHOU GAOPIN AUTOMATION EQUIPMENT Co.,Ltd. Registration number: Y2021980014104 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20220322 Granted publication date: 20171201 Pledgee: Hangzhou High-tech Financing Guarantee Co.,Ltd. Pledgor: HANGZHOU GAOPIN AUTOMATION EQUIPMENT Co.,Ltd. Registration number: Y2021980014104 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Turbine housing assembly test bench Effective date of registration: 20220322 Granted publication date: 20171201 Pledgee: Shanghai Guotai Junan Securities Asset Management Co.,Ltd. Pledgor: HANGZHOU GAOPIN AUTOMATION EQUIPMENT Co.,Ltd. Registration number: Y2022990000164 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230131 Granted publication date: 20171201 Pledgee: Shanghai Guotai Junan Securities Asset Management Co.,Ltd. Pledgor: HANGZHOU GAOPIN AUTOMATION EQUIPMENT Co.,Ltd. Registration number: Y2022990000164 |